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Determination of the effects of wind-induced vibration on cylindrical beamsThe objective of the analysis was to determine the critical length to diameter ratio (L/Do) of a hollow, cylindrical beam subjected to wind-induced vibration. The sizes of beams ranged from 4 to 24 inches and were composed of ASTM grade A and grade B and American Petroleum Institute grade X42 steels. Calculations used maximum steady-state wind speeds of 130 mph associated with hurricane conditions possible at the Kennedy Space Center. The study examined the effect that different end support and load conditions have on the natural frequencies of the beams. Finally, methods of changing the frequency of the wind-induced vibration were examined. The conclusions drawn were that the greatest possible L/Do is achieved using welded supports and limiting the maximum applied axial and bending loads to less than 50 percent.
Document ID
19920003082
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Artusa, E. A.
(NASA John F. Kennedy Space Center Cocoa Beach, FL, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1991
Subject Category
Structural Mechanics
Report/Patent Number
KSC-DM-3538
NASA-TM-103824
NAS 1.15:103824
Report Number: KSC-DM-3538
Report Number: NASA-TM-103824
Report Number: NAS 1.15:103824
Accession Number
92N12300
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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